STC SA00668SE

Supplemental type certificate · Micro AeroDynamics Inc

Holder
Micro AeroDynamics Inc · United States
Status
Current · Amended
Status date
June 12, 2009
Applied
October 1, 1998
Product
Aircraft · Single-Engine
Certification basis
Part 21, Part 23
Data sheet
TCDSA22NM

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

Installation of vortex generators on the wing leading edge and underside of the horizontal stabilizer.

What the certificate says

From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.

Number SA00668SE This certificate, issued to Micro AeroDynamics, Inc.

4000 Airport Road, Suite D Anacortes, WA 98221

Part 23 of the Federal Aviation Regulations.

Original Product ⎯Type Certificate Number: A22NM Make: Aviat Model: Husky A-1, A-1A, A-1B, A-1C-180, A-1C-200

Description of the Type Design Change: Installation of vortex generators on the wing leading edge and underside of the horizontal stabilizer, in accordance with Micro AeroDynamics Drawing List MA2089, Rev B, dated May 8, 2009, and Installation Manual MA2090, Rev B, dated May 8, 2009, or later FAA approved revisions.

NOTE: If more than five vortex generators are damaged or missing, the aircraft is not airworthy.

Limitations and Conditions: Approval of this change in type design applies to the above model aircraft only.

This approval should not be extended to other aircraft on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and any other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft. Additionally, if more than 5 vortex generators are damaged or missing, the aircraft is not to be considered airworthy. A copy of this certificate must be maintained as part of the permanent records for the modified aircraft.

If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

This certificate and the supporting data which is the basis for a pproval shall remain in effect until surrendered, suspended, revoked, or a termination date is otherwise established by the Administrator of the Federal Aviation Administration.

Date of application: October 1, 1998 Date reissued:

Date of issuance: February 17, 1999 Date amended: October 15, 1999, June 12, 2009

(Signature) Manager, Seattle Aircraft Certification Office (Title)

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 5

MakeModelData sheet
Sky International Inc.A-1A22NM
Sky International Inc.A-1AA22NM
Sky International Inc.A-1BA22NM
Sky International Inc.A-1C-180A22NM
Sky International Inc.A-1C-200A22NM